FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement) |   | 97% |   | 75% | 1 | 3 | 2 | 58 | 0 | 1 |
FieldEquinoctialOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngle, Frame, FieldAbsoluteDate, CalculusFieldElement) |   | 94% |   | 83% | 2 | 9 | 2 | 43 | 0 | 1 |
addKeplerContribution(PositionAngle, CalculusFieldElement, CalculusFieldElement[]) |  | 96% |   | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
computeJacobianMeanWrtCartesian() |  | 100% | | n/a | 0 | 1 | 0 | 57 | 0 | 1 |
computePVWithoutA() |  | 100% |  | 100% | 0 | 2 | 0 | 35 | 0 | 1 |
interpolate(FieldAbsoluteDate, Stream) |  | 100% |  | 100% | 0 | 7 | 0 | 39 | 0 | 1 |
nonKeplerianAcceleration() |  | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
computeJacobianTrueWrtCartesian() |  | 100% |  | 100% | 0 | 2 | 0 | 23 | 0 | 1 |
shiftedBy(CalculusFieldElement) |  | 100% |  | 100% | 0 | 2 | 0 | 17 | 0 | 1 |
meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% |   | 75% | 1 | 3 | 0 | 15 | 0 | 1 |
toOrbit() |  | 100% |  | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
computeJacobianEccentricWrtCartesian() |  | 100% |  | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
FieldEquinoctialOrbit(FieldOrbit) |  | 100% | | n/a | 0 | 1 | 0 | 17 | 0 | 1 |
eccentricToTrue(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
trueToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
initPVCoordinates() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
toString() |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getIDot() |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getLMDot() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getLEDot() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getEDot() |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getI() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
FieldEquinoctialOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngle, Frame, FieldAbsoluteDate, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
eccentricToMean(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getE() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getL(PositionAngle) |  | 100% |  | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getLDot(PositionAngle) |  | 100% |  | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getLM() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
shiftedBy(double) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
FieldEquinoctialOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLE() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
hasDerivatives() |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getADot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHxDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLvDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |